4027 - COMPARISON OF DOUBLE AND SINGLE BONDED REPAIRS TO SYMMETRIC COMPOSITE STRUCTURES: A NUMERICAL ANALYSIS

Owing to the importance of crack patching in fracture mechanics analysis, the aim of this study is to analyse numerically by the finite element method the advantage of the use of the bonded symmetric composite patch for repairing cracks in metallic sheets in mode I and mixed mode. The obtained results show that there is a considerable reduction of the asymptotic value of the stress intensity factor at the crack tip in the case of the use of the double symmetric patch compared with the single patch. In addition the gain of the composite thickness obtained by the double patch is also considerable in both mode one and mixed mode.

[1]  R. J. Callinan,et al.  Finite Element Analysis of an F-111 Lower Wing Skin Fatigue Crack Repair. , 1997 .

[2]  Wing Kong Chiu,et al.  Composite repairs to rib stiffened panels , 1999 .

[3]  M. Belhouari,et al.  Computation of the stress intensity factors for repaired cracks with bonded composite patch in mode I and mixed mode , 2002 .

[4]  Turaga V.R.S. Umamaheswar,et al.  Modelling of a patch repair to a thin cracked sheet , 1999 .

[5]  Wen-Hwa Chen,et al.  Estimation of stress intensity factors in partially patched cracked composite laminates by multilayer hybrid-stress finite element method , 1995 .

[6]  Shankar Mall,et al.  Modeling of a cracked metallic structure with bonded composite patch using the three layer technique , 1996 .

[7]  W. Chiu,et al.  Composite repairs to cracks in thick metallic components , 1999 .

[8]  B. B. Bouiadjra,et al.  Computation of the stress intensity factor for patched crack with bonded composite repair in pure mode II , 2003 .

[9]  S. Mall,et al.  Modeling of cracked thick metallic structure with bonded composite patch repair using three-layer technique , 1999 .

[10]  C. Sun,et al.  Characterization of Fatigue Behavior of Bonded Composite Repairs , 1999 .

[11]  D. Ouinas,et al.  Numerical analysis of the performances of the bonded composite patch for reducing stress concentration and repairing cracks at notch , 2003 .

[12]  A. Baker Bonded composite repair of fatigue-cracked primary aircraft structure , 1999 .

[13]  R. D. Henshell,et al.  CRACK TIP FINITE ELEMENTS ARE UNNECESSARY , 1975 .

[14]  L. Rose An application of the inclusion analogy for bonded reinforcements , 1981 .